Systems and Methods for Implementing Flexible Members Including Integrated Tools Made from Metallic Glass-Based Materials
20190126674 ยท 2019-05-02
Assignee
Inventors
- Aaron Parness (Los Angeles, CA, US)
- Kalind C. Carpenter (Pasadena, CA, US)
- Douglas C. Hofmann (Altadena, CA)
Cpc classification
International classification
Abstract
Systems and methods in accordance with embodiments of the invention implement flexible members that include integrated tools made from metallic glass-based materials. In one embodiment, a structure includes: a flexible member characterized by an elongated geometry and an integrated tool disposed at one end of the elongated geometry; where the flexible member includes a metallic glass-based material.
Claims
1. A method of forming a flexible member including an integrated tool, comprising: forming a metallic glass-based material into a plurality of elongated geometries each having a first end and a second end and formed of a metallic glass-based material having a thickness of less than approximately three times the size of the plastic zone radius of the metallic glass-based material and an elastic limit of at least 1.0%; and deforming the elongated geometry to define at least one hook at a first end of the elongated geometry such that the elongated flexible member and the hook comprise a unitary body, wherein the temperature of the metallic glass-based material during deformation is lower than its respective crystallization temperature.
2. The method of claim 1, further comprising: attaching the second end of a plurality of elongated flexible members to a rotor element, such that each elongated flexible member is configured to at least partially wrap about the at least one rotor element during operation; and wherein the plurality of elongated flexible members are distributed around the at least one rotor element such that the aggregate of the plurality of elongated flexible members form an outer wheel of integrated tools about the at least one rotor element.
3. The method of claim 1, wherein the metallic glass-based material is a metallic glass matrix composite material.
4. The method of claim 1, wherein the metallic glass-based material is characterized by a fracture toughness of greater than approximately 80 MPa.Math.m.sup.1/2.
5. The method of claim 1, wherein the flexible metallic glass-based material is fully amorphous.
6. The method of claim 1, wherein the metallic glass-based material is characterized in that it has an elastic limit of greater than approximately 1.5%.
7. The method of claim 1, wherein the metallic glass-based material is characterized in that it has an elastic limit of greater than approximately 2%.
8. The method of claim 1, wherein the elongated flexible member is characterized by a thickness of less than approximately 1.5 mm.
9. The method of claim 1, wherein the elongated flexible member defines a plurality of extensions including a plurality of integrated tools disposed at one end of the respective extensions.
10. The method of claim 1, wherein the hook is defined by an angle of greater than approximately 80 relative to the remainder of the flexible member.
11. The method of claim 1, wherein forming the metallic glass-based material into an elongated geometry comprises shearing an elongated geometry from a sheet of the metallic glass-based material.
12. The method of claim 1, wherein the thickness of the elongated geometry is less than approximately three times the size of the plastic zone radius of the metallic glass-based material.
13. The method of claim 1, wherein deforming the elongated geometry comprises heating the elongate geometry and bending at least the first end thereof along the length thereof, wherein the temperature of the metallic-glass based material is around its respective glass transition temperature.
14. The method of claim 1, wherein the temperature of the metallic-glass based material during deforming is below its respective glass transition temperature.
15. A method of terrain traversing device comprising: forming a metallic glass-based material into a plurality of elongated geometries each having a first end and a second end and formed of a metallic glass-based material having a thickness of less than approximately three times the size of the plastic zone radius of the metallic glass-based material and an elastic limit of at least 1.0%; deforming the elongated geometry to define at least one hook at a first end of the elongated geometry such that the elongated flexible member and the hook comprise a unitary body, wherein the temperature of the metallic glass-based material during deformation is lower than its respective crystallization temperature; attaching the second end of a plurality of elongated flexible members to a rotor element, such that each elongated flexible member is configured to at least partially wrap about the at least one rotor element during operation; and wherein the plurality of elongated flexible members are distributed around the at least one rotor element such that the aggregate of the plurality of elongated flexible members form an outer wheel of integrated tools about the at least one rotor element.
16-20. (canceled)
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
[0035] Turning now to the drawings, systems and methods for implementing flexible members that include integrated tools made from metallic glass-based materials are illustrated. In many embodiments of the invention, the flexible members are elongated and include tools disposed at one end of its elongated geometry. In many embodiments, the integrated tool is a hook. In a number of embodiments, flexible members that include integrated hooks are disposed around the periphery of an annular rotor element. In numerous embodiments, either one or a plurality of such annular rotor elements are configured to operate as a wheel assembly.
[0036] For context,
[0037] Although configurations such as those depicted in
[0038] Metallic glasses, also known as amorphous alloys, embody a relatively new class of materials that is receiving much interest from the engineering and design communities. Metallic glasses are characterized by their disordered atomic-scale structure in spite of their metallic constituent elementsi.e. whereas conventional metallic materials typically possess a highly ordered atomic structure, metallic glass materials are characterized by their disordered atomic structure. Notably, metallic glasses typically possess a number of useful material properties that can allow them to be implemented as highly effective engineering materials. For example, metallic glasses are generally much harder than conventional metals, and are generally tougher than ceramic materials. They are also relatively corrosion resistant, and, unlike conventional glass, they can have good electrical conductivity. Importantly, metallic glass materials lend themselves to relatively easy processing in certain respects. For example, the forming of metallic glass materials can be compatible with injection molding processes. Thus, for example, metallic glass compositions can be cast into desired shapes.
[0039] Nonetheless, the practical implementation of metallic glasses presents certain challenges that limit their viability as engineering materials. In particular, metallic glasses are typically formed by raising a metallic alloy above its melting temperature, and rapidly cooling the melt to solidify it in a way such that its crystallization is avoided, thereby forming the metallic glass. The first metallic glasses required extraordinary cooling rates, e.g. on the order of 10.sup.6 K/s, and were thereby limited in the thickness with which they could be formed. Indeed, because of this limitation in thickness, metallic glasses were initially limited to applications that involved coatings. Since then, however, particular alloy compositions that are more resistant to crystallization have been developed, which can thereby form metallic glasses at much lower cooling rates, and can therefore be made to be much thicker (e.g. greater than 1 mm). These metallic glass compositions that can be made to be thicker are known as bulk metallic glasses (BMGs). As can be appreciated, such BMGs can be better suited for investment molding operations.
[0040] In addition to the development of BMGs, bulk metallic glass matrix composites (BMGMCs) have also been developed. BMGMCs are characterized in that they possess the amorphous structure of BMGs, but they also include crystalline phases of material within the matrix of amorphous structure. For example, the crystalline phases can exist in the form of dendrites. The crystalline phase inclusions can impart a host of favorable materials properties on the bulk material. For example, the crystalline phases can allow the material to have enhanced ductility, compared to where the material is entirely constituted of the amorphous structure. BMGs and BMGMCs can be referred to collectively as BMG-based materials. Similarly, metallic glasses, metallic glasses that include crystalline phase inclusions, BMGs, and BMGMCs can be referred to collectively as metallic glass-based materials or MG-based materials.
[0041] The potential of metallic glass-based materials continues to be explored, and developments continue to emerge. For example, in U.S. patent application Ser. No. 13/928,109, D. Hofmann et al. disclose the implementation of metallic glass-based materials in macroscale gears. The disclosure of U.S. patent application Ser. No. 13/928,109 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials, and their implementation in macroscale gears. Likewise, in U.S. patent application Ser. No. 13/942,932, D. Hofmann et al. disclose the implementation of metallic glass-based materials in macroscale compliant mechanisms. The disclosure of U.S. patent application Ser. No. 13/942,932 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials, and their implementation in macroscale compliant mechanisms. Moreover, in U.S. patent application Ser. No. 14/060,478, D. Hofmann et al. disclose techniques for depositing layers of metallic glass-based materials to form objects. The disclosure of U.S. patent application Ser. No. 14/060,478 is hereby incorporated by reference especially as it pertains to metallic glass-based materials, and techniques for depositing them to form objects. Furthermore, in U.S. patent application Ser. No. 14/163,936, D. Hofmann et al., disclose techniques for additively manufacturing objects so that they include metallic glass-based materials. The disclosure of U.S. patent application Ser. No. 14/163,936 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials, and additive manufacturing techniques for manufacturing objects so that they include metallic glass-based materials. Additionally, in U.S. patent application Ser. No. 14/177,608, D. Hofmann et al. disclose techniques for fabricating strain wave gears using metallic glass-based materials. The disclosure of U.S. patent application Ser. No. 14/177,608 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials, and their implementation in strain wave gears. Moreover, in U.S. patent application Ser. No. 14/178,098, D. Hofmann et al., disclose selectively developing equilibrium inclusions within an object constituted from a metallic glass-based material. The disclosure of U.S. patent application Ser. No. 14/178,098 is hereby incorporated by reference, especially as it pertains to metallic glass-based materials, and the tailored development of equilibrium inclusions within them. Furthermore, in U.S. patent application Ser. No. 14/252,585, D. Hofmann et al. disclose techniques for shaping sheet materials that include metallic glass-based materials, including using localized thermoplastic deformation and using cold working techniques. The disclosure of U.S. patent application Ser. No. 14/252,585 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials and techniques for shaping sheet materials that include metallic glass-based materials, including using localized thermoplastic deformation and using cold-working techniques. Additionally, in U.S. patent application Ser. No. 14/259,608, D. Hofmann et al. disclose techniques for fabricating structures including metallic glass-based materials using ultrasonic welding. The disclosure of U.S. patent application Ser. No. 14/259,608 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials and techniques for fabricating structures including metallic glass-based materials using ultrasonic welding. Moreover, in U.S. patent application Ser. No. 14/491,618, D. Hofmann et al. disclose techniques for fabricating structures including metallic glass-based materials using low pressure casting. The disclosure of U.S. patent application Ser. No. 14/491,618 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based materials and techniques for fabricating structures including metallic glass-based materials using low pressure casting. Furthermore, in U.S. patent application Ser. No. 14/660,730, Hofmann et al. disclose metallic glass-based fiber metal laminates. The disclosure of U.S. patent application Ser. No. 14/660,730 is hereby incorporated by reference in its entirety, especially as it pertains to metallic glass-based fiber metal laminates. Additionally, in U.S. patent application Ser. No. 14/971,848, A. Kennett et al. disclose techniques for manufacturing gearbox housings made from metallic glass-based materials. The disclosure of U.S. patent application Ser. No. 14/971,848, is hereby incorporated by reference in its entirety, especially as it pertains to the manufacture of metallic glass-based gearbox housings.
[0042] Notwithstanding all of these developments, the vast potential of metallic glass-based materials has yet to be fully appreciated. For instance, the suitability of metallic glass-based materials for implementation as flexible members that include integrated tools (e.g. the flexible suspension members microspine assemblies discussed in the '629 patent) has yet to be fully explored. Conventionally, the structures described in the '629 patent have been fabricated from conventional engineering metals like steel, nitinol, and/or polymers (as depicted in
Methods for Implementing Flexible Members Including Integral Tools from Metallic Glass-Based Materials
[0043] In many embodiments of the invention, flexible members including integral tools are fabricated from metallic glass-based materials. Any suitable manufacturing technique can be utilized to form the flexible member in accordance with embodiments of the invention. For example, in many embodiments, metallic glass-based materials are cold worked to shape them into the desired geometrye.g. they are shaped at temperatures less than or equal to approximately room temperature (e.g. 72 F.). More broadly stated, cold-working can be said to occur when an MG-based material is shaped at a temperature less than its respective glass transition temperature. Thus for instance,
[0044] While cold-working a flexible member to form an integrated tool from a metallic glass-based material has been illustrated, it should be clear that any of a variety of processes can be implemented to form a flexible member including an integrated tool in accordance with embodiments of the invention. For example, in many embodiments, localized thermoplastic deformation processes as disclosed in U.S. patent application Ser. No. 14/252,585 incorporated by reference above are implemented, e.g. the flexible member can be bent when a region of the flexible member is above its respective glass transition temperature to define the hook. In many embodiments, direct casting techniques are utilized; casting can be a particularly efficient manufacturing strategy for the bulk fabrication of the described structures. Any suitable manufacturing technology can be implemented in accordance with embodiments of the invention.
[0045] Moreover, note that any suitable MG-based composition can be utilized to form a flexible member having an integrated tool in accordance with embodiments of the invention; embodiments of the invention are not limited to a particular composition. For example, in many instances, the utilized alloy composition is a composition that is based on one of: Ti, Zr, Cu, Ni, Fe, Pd, Pt, Ag, Au, Al, Hf, W, TiZrBe, CuZr, ZrBe, TiCu, ZrCuNiAl, TiZrCuBe and combinations thereof. In the instant context, the term based on can be understood to mean that the specified element(s) are present in the greatest amount relative to any other present elements. Additionally, within the context of the instant application, the term MG-based composition can be understood reference an element, or aggregation of elements, that are capable of forming a metallic glass-based material (e.g. via being exposed to a sufficiently rapid, but viable, cooling rate). While several examples of suitable metallic glass-based materials are listed above, it should be reiterated that any suitable metallic glass-based composition can be incorporated in accordance with embodiments of the invention; for example, any of the metallic glass-based compositions listed in the disclosures cited and incorporated by reference above can be implemented. As alluded to above, in many embodiments, the implemented MG-based composition is based on the manufacturing technique to be applied. For example, where cold working will be used to shape the MG-based composition, a MG-based composition that is capable of forming a MG-based material characterized by a relatively high fracture toughness can be implemented. In a number of embodiments, the MG-based material is characterized by a fracture toughness of greater than approximately 80 MPa.Math.m.sup.1/2. In several embodiments, the MG-based material is characterized by a fracture toughness of greater than approximately 100 MPa.Math.m.sup.1/2. In many embodiments, the MG-based composition is implemented in the form of a matrix composite characterized by a particularly high fracture toughness (e.g. greater than approximately 80 MPa.Math.m.sup.1/2 or approximately 100 MPa.Math.m.sup.1/2). In a number of embodiments, the MG-based material that is to be formed into a flexible member via cold-forming is characterized by a thickness that is less than approximately three times the thickness of the plastic zone radius of the respective MG-based material. In numerous embodiments, the MG-based material that is to be formed into a flexible member via cold-forming is characterized by a thickness that is less than plastic zone radius of the respective MG-based material. In several embodiments, the MG-based material is characterized by a thickness of less than approximately 1.5 mm. These thicknesses can facilitate the desired formability. In many instances, the particular MG-based composition to be implemented is based on an assessment of the anticipated operating environment for the flexible member. For example, where it desired that the flexible member be relatively less massive, a titanium based MG-based material can be implemented. In many instances, the selection of the MG-based material to be implemented is based on the desire for one of: environmental resilience, toughness, wear resistance, hardness, density, machinability, and combinations thereof. In numerous embodiments, the MG-based material to be implemented is based on the desire to have relatively high resistance to wear (which can be correlated with hardness) and relatively high flexibility (which can be correlated with elastic strain limit). In many embodiments, the hardness of the MG-based material to be implemented is characterized by a value greater than approximately 50 Rc according to the Rockwell scale. In a number of embodiments, the MG-based material to be implemented has an elastic limit greater than approximately 1%. For reference, Tables 1-6 list materials data that can be relied on in selecting a metallic glass-based composition to be implemented. Any suitable MG-based material listed in the tables below can be implemented in accordance with various embodiments of the invention.
TABLE-US-00001 TABLE 1 Material Properties of MG-Based Materials relative to Heritage Engineering Materials Density Stiffness, E Tensile Yield Tensile UTS Elastic Limit Specific Hardness Material (g/cc) (GPa) (MPa) (MPa) (%) Strength (HRC) SS 15500 H1024 7.8 200 1140 1170 <1 146 36 Ti6Al4V STA 4.4 114 965 1035 <1 219 41 Ti6Al6V4Sn STA 4.5 112 1035 1100 <1 230 42 Nitronic 60 CW 7.6 179 1241 1379 <1 163 40 Vascomax C300 8.0 190 1897 1966 <1 237 50 Zr-BMG 6.1 97 1737 1737 >1.8 285 60 Ti-BMGMC 5.2 94 1362 1429 >1.4 262 51 Zr-BMGMC 5.8 75 1096 1210 >1.4 189 48
TABLE-US-00002 TABLE 2 Material Properties of Select MG-Based Materials as a function of Composition BMG bcc .sub.y .sub.max .sub.y E T.sub.x name atomic % weight % (%) (%) (g/cm.sup.3) (MPa) (MPa) (%) (GPa) (K) DV2 Ti.sub.44Zr.sub.20V.sub.12Cu.sub.5Be.sub.15 Ti.sub.41.9Zr.sub.35.3V.sub.12.1Cu.sub.6.3Be.sub.3.4 70 30 5.13 1597 1614 2.1 94.5 956 DV1 Ti.sub.48Zr.sub.30V.sub.12Cu.sub.5Be.sub.15 Ti.sub.44.3Zr.sub.35.2V.sub.11.8Cu.sub.6.1Be.sub.2.6 53 47 5.15 1362 1429 2.3 9.2 955 DV3 Ti.sub.56Zr.sub.18V.sub.10Cu.sub.4Be.sub.12 Ti.sub.51.6Zr.sub.31.6V.sub.9.8Cu.sub.4.9Be.sub.2.1 46 54 5.08 1308 1309 2.2 84.0 951 DV4 Ti.sub.62Zr.sub.15V.sub.10Cu.sub.4Be.sub.9 Ti.sub.57.3Zr.sub.26.4V.sub.9.8Cu.sub.4.9Be.sub.1.6 40 60 5.03 1086 1089 2.1 83.7 940 DVAl1 Ti.sub.60Zr.sub.16V.sub.9Cu.sub.3Al.sub.3Be.sub.9 Ti.sub.55.8Zr.sub.38.4V.sub.8.9Cu.sub.3.7Al.sub.1.6Be.sub.1.5 31 69 4.97 1166 1189 2.0 84.2 901 DVAl2 Ti.sub.67Zr.sub.11V.sub.10Cu.sub.5Al.sub.2Be.sub.2 Ti.sub.54.2Zr.sub.39.5V.sub.9.5Cu.sub.6.2Al.sub.1Be.sub.0.5 20 80 4.97 990 1000 2.0 78.7 998 Ti-6-4a Ti.sub.86.1Al.sub.10.3V.sub.3.6 Ti.sub.90Al.sub.6V.sub.4 (Grade 5 Annealed) na na 4.43 754 882 1.0 113.8 1877 Ti-6-4s Ti.sub.86.1Al.sub.10.3V.sub.3.5 [Ref] Ti.sub.98Al.sub.6V.sub.4 (Grade 5 STA) na na 4.43 1100 1170 1 114.0 1877 CP-Ti Ti.sub.100 Ti.sub.100 (Grade 2) na na 4.51 380 409 0.7 105.0 1930
TABLE-US-00003 TABLE 3 Material Properties of Select MG-Based Materials as a function of Composition .sub.max E.sub.lot .sub.y .sub.y E G CIT RoA Alloy (MPa) (%) (MPa) (%) (GPa) (g/cm.sup.3) (GPa) (J) (%) Zr.sub.36.6Ti.sub.31.4Nb.sub.7Cu.sub.5.9Be.sub.19.1 (DH1) 1512 9.58 1474 1.98 84.3 5.6 30.7 26 44 0.371 Zr.sub.38.3Ti.sub.32.9Nb.sub.7.3Cu.sub.6.2Be.sub.15.3 (DH2) 1411 10.0 1567 1.92 79.2 5.7 28.8 40 50 0.373 Zr.sub.39.6Ti.sub.33.9Nb.sub.7.6Cu.sub.6.4Be.sub.12.5 (DH3) 1210 13.10 1096 1.62 75.3 5.8 27.3 45 46 0.376 Zr.sub.41.2Ti.sub.13.8Cu.sub.12.5Ni.sub.10Be.sub.22.5 (Vitreloy 1) 1737 1.98 97.2 6.1 35.9 8 0 0.355 Zr.sub.56.2Ti.sub.13.8Nb.sub.5.0Cu.sub.6.9Ni.sub.5.6Be.sub.12.5 (LM2) 1302 5.49 1046 1.48 78.8 6.2 28.6 24 22 0.375
TABLE-US-00004 TABLE 4 Material Properties as a Function of Composition and Structure, where A is Amorphous, X, is Crystalline, and C is Composite A/X/C 2.0Hv E (GPa) (CuZr.sub.42Al.sub.7Be.sub.10)Nb.sub.3 A 626.5 108.5 (CuZr.sub.46Al.sub.5Y.sub.2)Nb.sub.3 A 407.4 76.9 (CuZrAl.sub.7Be.sub.5)Nb.sub.3 A 544.4 97.8 (CuZrAl.sub.7Be.sub.7)Nb.sub.3 A 523.9 102.0 Cu.sub.40Zr.sub.40Al.sub.10Be.sub.10 A 604.3 114.2 Cu.sub.41Zr.sub.40Al.sub.7Be.sub.7Co.sub.5 C 589.9 103.5 Cu.sub.42Zr.sub.41Al.sub.7Be.sub.7Co.sub.3 A 532.4 101.3 Cu.sub.47.5Zr.sub.48Al.sub.4Co.sub.0.5 X 381.9 79.6 Cu.sub.47Zr.sub.46Al.sub.5Y.sub.2 A 409.8 75.3 Cu.sub.50Zr.sub.50 X 325.9 81.3 CuZr.sub.41Al.sub.7Be.sub.7Cr.sub.3 A 575.1 106.5 CuZrAl.sub.5Be.sub.5Y.sub.2 A 511.1 88.5 CuZrAl.sub.5Ni.sub.3Be.sub.4 A 504.3 95.5 CuZrAl.sub.7 X 510.5 101.4 CuZrAl.sub.7Ag.sub.7 C 496.1 90.6 CuZrAl.sub.7Ni.sub.5 X 570.0 99.2 Ni.sub.40Zr.sub.28.5Ti.sub.16.5Be.sub.15 C 715.2 128.4 Ni.sub.40Zr.sub.28.5Ti.sub.16.5Cu.sub.15Al.sub.10 X 627.2 99.3 Ni.sub.40Zr.sub.28.5Ti.sub.16.5Cu.sub.15Be.sub.10 C 668.2 112.0 Ni.sub.56Zr.sub.17Ti.sub.13Si.sub.2Sn.sub.3Be.sub.9 X 562.5 141.1 Ni.sub.56Zr.sub.18Ti.sub.14Si.sub.2Sn.sub.3Be.sub.6 X 637.3 139.4 Ti.sub.33.18Zr.sub.30.51Ni.sub.5.33Be.sub.22.88Cu.sub.8.1 A 486.1 96.9 Ti.sub.40Zr.sub.25Be.sub.30Cr.sub.5 A 465.4 97.5 Ti.sub.40Zr.sub.25Ni.sub.8Cu.sub.9Be.sub.18 A 544.4 101.1 Ti.sub.45Zr.sub.16Ni.sub.9Cu.sub.10Be.sub.20 A 523.1 104.2 Vit 1 A 530.4 95.2 Vit 105 (Zr.sub.52.5Ti.sub.5Cu.sub.17.9Ni.sub.14.6Al.sub.10) A 474.4 88.5 Vit 106 A 439.7 83.3 Zr.sub.55Cu.sub.30Al.sub.10Ni.sub.5 A 520.8 87.2 Zr.sub.65Cu.sub.17.5Al.sub.7.5Ni.sub.10 A 463.3 116.9 DH1 C 391.1 84.7 GHDT (Ti.sub.30Zr.sub.35Cu.sub.8.2Be.sub.26.8) A 461.8 90.5
TABLE-US-00005 TABLE 5 Fatigue Characteristics as a Function of Composition Fracture Fatigue Strength Geometry Loading Frequency Limit Fatigue Material (MPa) (mm) mode (Hz) R-ratio (MPa) ratio Zr.sub.56.2Cu.sub.6.9Ni.sub.5.6Ti.sub.13.8Nb.sub.5.0Be.sub.12.5 1480 3 3 30 4PB 25 0.1 ~296 0.200 Composites Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1900 3 3 50 4PB 25 0.1 ~152 0.080 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1900 2 2 60 3PB 10 0.1 768 0.404 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1900 2 2 60 3PB 10 0.1 359 0.189 Zr.sub.44Ti.sub.11Ni.sub.10Cu.sub.10Be.sub.25 1900 2.3 2.0 85 4PB 5-20 0.3 550 0.289 Zr.sub.44Ti.sub.11Ni.sub.10Cu.sub.10Be.sub.25 1900 2.3 2.0 85 4PB 5-20 0.3 390 0.205 Zr.sub.52.5Cu.sub.17.9Al.sub.10Ni.sub.14.6Ti.sub.5 1700 3.5 3.5 30 4PB 10 0.1 850 0.500 (Zr.sub.58Ni.sub.13.6Cu.sub.18Al.sub.10.4).sub.99Nb.sub.1 1700 2 2 25 4PB 10 0.1 559 0.329 Zr.sub.55Cu.sub.30Ni.sub.5Al.sub.10 1560 2 20 50 Plate 40 0.1 410 0.263 bend
TABLE-US-00006 TABLE 6 Fatigue Characteristics as a Function of Composition Fracture Fatigue Strength Geometry Loading Frequency Limit Fatigue Material (MPa) (mm) mode (Hz) R-ratio (MPa) ratio Zr.sub.56.2Cu.sub.6.9Ni.sub.5.6Ti.sub.13.8Nb.sub.5.0Be.sub.12.5 1480 02.98 TT 10 0.1 239 0.161 Composites Zr.sub.55Cu.sub.30Al.sub.10Ni.sub.5 Nano 1700 2 4 70 TT 10 0.1 ~340 0.200 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1850 2.98 TT 10 0.1 703 0.380 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1850 2.98 TT 10 0.1 615 0.332 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1850 2.98 TT 10 0.1 567 0.306 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1900 CC 5 0.1 ~1050 0.553 Zr.sub.41.2Cu.sub.12.5Ni.sub.10Ti.sub.13.8Be.sub.22.5 1900 TC 5 ~1 ~150 0.079 Zr.sub.50Cu.sub.40Al.sub.10 1821 2.98 TT 10 0.1 752 0.413 Zr.sub.50Cu.sub.30Al.sub.10Ni.sub.10 1900 2.98 TT 10 0.1 865 0.455 Zr.sub.50Cu.sub.30Al.sub.10Pd.sub.3 1899 2.98 TT 10 0.1 983 0.518 Zr.sub.50Cu.sub.30Al.sub.10Pd.sub.3 1899 2.98 TT 10 0.1 ~900 0.474 Zr.sub.52.5Cu.sub.17.9Al.sub.10Ni.sub.14.6Ti.sub.5 1660 6 3 15 TT 1 0.1 Zr.sub.52.5Cu.sub.17.9Al.sub.10Ni.sub.14.6Ti.sub.5 1700 2.98 TT 10 0.1 907 0.534 Zr.sub.59Cu.sub.20Al.sub.10Ni.sub.8Ti.sub.3 1580 6 3 1.5 TT 1 0.1 Zr.sub.65Cu.sub.15Al.sub.10Ni.sub.10 1300 3 4 16 TT 20 0.1 ~280 0.215 Zr.sub.55Cu.sub.30Al.sub.10Ni.sub.5 1560 1 2 5 TT 0.13 0.5
[0046] Furthermore, although a particular geometry for a flexible member with an integrated tool is illustrated and described with respect to
[0047] In many embodiments, the flexible members described above are incorporated within the context of a terrain traversing vehicle as disclosed in the terrain traversing devices disclosed in the '629 application. Thus, for example,
[0048] Notably, metallic glass-based materials are often characterized by their high elastic limits. For example, whereas conventional metals have elastic limits on the order of 1%, metallic glass-based materials can have elastic limits as high as 2% or more. This high elasticity can allow them to be viably implemented within the terrain traversing devices disclosed in the '629 patent.
[0049]
[0050]
[0051] As can be inferred from the above discussion, the above-mentioned concepts can be implemented in a variety of arrangements in accordance with embodiments of the invention. For example, while a hook has been given as the example of an integrated tool, any suitable integrated tool can be implemented in accordance with embodiments of the invention. For instance, any implement configured to facilitate mobility or grip/engage a surface can be implemented. Accordingly, although the present invention has been described in certain specific aspects, many additional modifications and variations would be apparent to those skilled in the art. It is therefore to be understood that the present invention may be practiced otherwise than specifically described. Thus, embodiments of the present invention should be considered in all respects as illustrative and not restrictive.